KUIPER-00413, 68928
Orbit data source: Space-Track
KUIPER-00413, 68928 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 30 Apr 2026 UTC via an ARIANE 64 launch vehicle from the French Guiana (FRGUI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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68928 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational spacecraft
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 3.4 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00413
1 68928U 26098K 26171.39303836 -.00266273 00000-0 -99718-2 0 9994
2 68928 51.8774 54.1776 0019519 148.7794 211.4352 15.27690758 7816Epoch: 2026-06-20T09:25Z
TLE epoch observation values (Epoch: 2026-06-20T09:25:58.514Z)
Latitude
-0.00003°
Longitude
4.07546°
Altitude
494.911 km
Speed
7.612 km/s
True Right ascension
03h 36m 42s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:20:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.574 km
Perigee altitude
469.789 km
Semi-major axis
6,861.319 km
Eccentricity
0.00195
Inclination
51.8774°
RAAN
54.1776°
Arg. of periapsis
148.7794°
True anomaly
211.31879°
Mean anomaly
211.4352°
Eccentric anomaly
211.37697°
Mean motion
3.81884 °/min
Orbital period
94.27 mins
BSTAR
-0.0099718
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Other satellites on launch #98 in the year 2026 (2026-04-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.KUIPER-00413 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 20:40:32.421Z | 283.482° WNW | 2026-06-20 20:43:32.421Z | 337.745° N | 21.245° | 2026-06-20 20:45:32.421Z | 20.089° NNE |
| 4 mins | 2026-06-21 00:00:32.421Z | 346.363° N | 2026-06-21 00:02:32.421Z | 28.624° NE | 18.196° | 2026-06-21 00:04:32.421Z | 63.984° ENE |
| 5 mins | 2026-06-21 01:38:32.421Z | 309.584° NW | 2026-06-21 01:40:32.421Z | 327.59° NNW | 44.237° | 2026-06-21 01:43:32.421Z | 126.508° SE |
| 5 mins | 2026-06-21 18:36:32.421Z | 212.594° SW | 2026-06-21 18:38:32.421Z | 116.825° SE | 41.658° | 2026-06-21 18:41:32.421Z | 58.665° ENE |
| 4 mins | 2026-06-21 20:15:32.421Z | 305.632° NW | 2026-06-21 20:16:32.421Z | 329.1° NNW | 21.947° | 2026-06-21 20:19:32.421Z | 29.153° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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